Photo from the personal collection of Konstantinos Panitsidis


 Technical specifications      Photos      Video

 

 

Designers: Motor Sich, JSC Zaporozhye, Ukraine
Manufacturer: Motor Sich, JSC Zaporozhye, Ukraine

The MS-14VM engine is a turboshaft version of the MS-14 engine. The engine can be used as a power plant for medium-class helicopters and for retrofitting of Mi-8T helicopters.

 


TECHNICAL SPECIFICATIONS

Fuel -
Oil -
Propeller shaft power, take-off power rating 1.600 h.p.
Specific fuel consumption, take-off power rating 0,240 kg/eshp. h
Propeller shaft power, cruise power 1.100 h.p. (H=0.0 m, M=0.0, ISA +25oC)
Specific fuel consumption, cruise power 0,265 kg/eshp. h
Pressure ratio, take-take-off power rating -
Temperature of the gas at the turbine intake, take-off power rating -
Air flow rate, take-off power rating -
Compressor rotation frequency low-pressure, take-off power rating -
Diameter -
Height -
Width -
Lenght -
Weight 310+10 kg
Specified service life -

 


PHOTOS MS-14VM